CN110243521A - A kind of sheet stress measurement method and sheet stress measuring system - Google Patents
A kind of sheet stress measurement method and sheet stress measuring system Download PDFInfo
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- CN110243521A CN110243521A CN201910590675.9A CN201910590675A CN110243521A CN 110243521 A CN110243521 A CN 110243521A CN 201910590675 A CN201910590675 A CN 201910590675A CN 110243521 A CN110243521 A CN 110243521A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/0028—Force sensors associated with force applying means
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/02—Details not specific for a particular testing method
- G01N2203/06—Indicating or recording means; Sensing means
- G01N2203/067—Parameter measured for estimating the property
- G01N2203/0676—Force, weight, load, energy, speed or acceleration
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Abstract
The present invention discloses a kind of sheet stress measurement method, obtains the thin plate duplicate of in-service thin plate, thin plate duplicate and in-service thin plate shape having the same and material；Loading experiment is made to thin plate duplicate, according to Lamb wave SiZero group velocity resonant frequency of mode and the relationship for applying stress obtain Lamb wave SiZero group velocity of duplicate mode-stress parameters；After obtaining thin plate duplicate, under conditions of not destroying in-service thin plate, Lamb wave is motivated to a certain detection zone of in-service thin plate, and the receiving point near excitation point obtains Lamb wave and acquires signal；Lamb wave acquisition signal is handled, the in-service resonant frequency S of zero group velocity of Lamb wave mode is obtainedif, according to the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate mean stress suffered by in-service thin plate detection zone.The mean stress that signal calculates in-service thin plate particular detection region is acquired according to the Lamb wave of the related data of loading experiment and in-service thin plate, in-service thin plate original state is kept, does not influence the normal condition of thin plate.
Description
Technical field
The present invention relates to stress measurement technical fields, further relate to a kind of sheet stress measurement method.In addition, this hair
It is bright to further relate to a kind of sheet stress measuring system.
Background technique
Thin-plate element is widely used in aerospace industry, auto industry, shipping industry, pressure boiler, large-size chemical container etc.
Field, during long-time is on active service, thin-plate element undergoes different type, the effect of different size of load, in thin-plate element
It is inevitably generated stress collection and neutralizes stresses re-distribution phenomenon, if corresponding solution cannot be detected in time and be used,
It may cause structure function and be abnormal and even fail, cause casualties and property loss.
Traditional method for measuring stress generallys use Blind Hole Method, ring core method, and such measurement method belongs to destructive measurement side
Method, detection process needs to remove the sub-fraction of test object, and the detection of the nondestructive determinations such as X-ray and neutron diffraction method is set
Standby prohibitively expensive complexity, these methods are not suitable for the absolute stress field measurement of in-service sheet metal,
For those skilled in the art, a kind of lossless detection method how is designed, thin-plate element is not being destroyed
In the case of, the stress of in-service thin plate is measured, is the technical issues that need to address a few days ago.
Summary of the invention
The present invention provides a kind of sheet stress measurement method, by carrying out loading experiment to thin plate duplicate, utilizes blue nurse
Wave measures the stress of in-service thin plate under conditions of not destroying in-service thin plate, and concrete scheme is as follows:
A kind of sheet stress measurement method, comprising:
S1, the thin plate duplicate for obtaining in-service thin plate, the thin plate duplicate and the in-service thin plate are having the same outer
Shape and material；
S2, loading experiment is made to the thin plate duplicate, according to Lamb wave SiZero group velocity resonant frequency of mode and application are answered
The relationship of power obtains Lamb wave SiZero group velocity of duplicate mode-stress parameters；
S3, it is acquired to a certain area excitation Lamb wave of in-service thin plate, and motivating the receiving point near point to obtain Lamb wave
Signal；
S4, Lamb wave acquisition signal is handled, obtains the in-service resonant frequency S of zero group velocity of Lamb wave modeif, root
According to the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate mean stress suffered by in-service thin plate detection zone.
Optionally, further includes:
S5, mean stress is computed repeatedly to the different detection zones of in-service thin plate, describes the Stress Field Distribution of in-service thin plate
Figure.
Optionally, loading experiment step S2, is made to the thin plate duplicate, obtains Lamb wave SiDuplicate mode zero group
Speed-stress parameters, comprising:
S21, Lamb wave signal is motivated to the thin plate duplicate in excitation point, connecing in excitation twice of wave-length coverage of point
Sink acquires Lamb wave time-domain signal；
S22, Hanning window function is added to the Lamb wave time-domain signal, and carries out Fast Fourier Transform, obtain blue nurse
Wave frequency domain signal waveforms；Lamb wave S is extracted from the Lamb wave frequency-region signal waveform diagramiZero group velocity of mode adds outside in nothing answers
The thin plate duplicate corresponding Lamb wave S when poweriZero group velocity resonant frequency of mode；
S23, simple stress of different sizes is applied several times to the thin plate duplicate, the simple stress is answered in elasticity
Within the scope of power；After the simple stress reaches stable state, Lamb wave S under each simple stress is obtainediThe resonance of zero group velocity of mode
Frequency；
S24, with Lamb wave SiZero group velocity resonant frequency of mode is abscissa, and simple stress is ordinate, establishes Descartes
Coordinate system；By the simple stress and corresponding Lamb wave SiThe corresponding coordinate points of zero group velocity resonant frequency of mode substitute into coordinate system
In, and linear fit is carried out to coordinate points, obtained straight slope K is the Lamb wave SiZero group velocity of duplicate mode-stress
The intersection point of parameter, straight line and axis of abscissas is constant C.
Optionally, when making loading experiment to the thin plate duplicate, excitation point and the line of receiving point are answered with the single shaft
The direction of power is parallel.
Optionally, step S4, Lamb wave acquisition signal is handled, according to Lamb wave SiThe resonance of zero group velocity of mode
Frequency calculates mean stress suffered by in-service thin plate detection zone, comprising:
S41, Hanning window function is added to Lamb wave acquisition signal, and carries out Fast Fourier Transform, obtain blue nurse
Wave SiLamb wave mode zero group velocity in-service resonant frequency S of zero group velocity of mode in in-service thin plate detection zoneif；
S42, according to the straight slope K, the constant C, the in-service resonant frequency S of zero group velocity of Lamb wave modeif, benefit
The mean stress of in-service thin plate detection zone is calculated with following formula:
σ=KSif-C
Wherein, σ is mean stress.
The present invention also provides a kind of sheet stress measuring system, including the function generator for emitting pulse electrical signal,
The pulse electrical signal of the function generator transmitting is broadcast to P wave emission probe after the processing of ultrasonic preamplifier, described
P wave emission probe emits longitudinal wave to thin plate at an angle by angle modifying wedges；
Longitudinal wave receiving transducer receives the Lamb wave of thin plate, and it is aobvious to be sent to oscillograph after the processing of ultrasonic post amplifier
Show, and by processing module calculation processing；
The processing module can be according to Lamb wave SiZero group velocity resonant frequency of mode and the relationship for applying stress obtain blue
Nurse wave SiZero group velocity of duplicate mode-stress parameters；And Lamb wave acquisition signal is handled, obtain Lamb wave mode
The in-service resonant frequency S of zero group velocityif, according to the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate in-service thin plate detection
Mean stress suffered by region；Mean stress is computed repeatedly to the different detection zones of in-service thin plate, describes answering for in-service thin plate
Force distribution figure；
It further include the stretching-machine for applying simple stress to thin plate duplicate.
Optionally, the distance between the P wave emission probe and the longitudinal wave receiving transducer are less than or equal to twice of wave
It is long.
Core of the invention is to provide a kind of sheet stress measurement method, obtains the thin plate duplicate of in-service thin plate, thin
Plate duplicate and in-service thin plate shape having the same and material；Loading experiment is made to thin plate duplicate, according to Lamb wave SiMould
Zero group velocity resonant frequency of state and the relationship for applying stress obtain Lamb wave SiZero group velocity of duplicate mode-stress parameters；It obtains thin
After plate duplicate, under conditions of not destroying in-service thin plate, Lamb wave is motivated to a certain detection zone of in-service thin plate, and swashing
It encourages the receiving point near a little and obtains Lamb wave acquisition signal；Lamb wave acquisition signal is handled, Lamb wave mode zero is obtained
The in-service resonant frequency S of group velocityif, according to the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate in-service thin plate detection zone institute
The mean stress received.The present invention only carries out loading experiment to thin plate duplicate, according to the related data of loading experiment and in-service thin
The Lamb wave acquisition signal of plate calculates the mean stress in in-service thin plate particular detection region, does not influence the normal condition of thin plate.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with
It obtains other drawings based on these drawings.
Fig. 1 is the flow chart of sheet stress measurement method of the present invention；
Frequency-domain waveform figure of the Fig. 2 between frequency and amplitude；
Fig. 3 is the structural schematic diagram of sheet stress measuring system of the present invention.
Include: in figure
Function generator 1, ultrasonic preamplifier 2, P wave emission probe 3, angle modifying wedges 4, longitudinal wave receiving transducer
5, ultrasonic post amplifier 6, oscillograph 7, processing module 8, stretching-machine 9.
Specific embodiment
Core of the invention is to provide a kind of sheet stress measurement method, real by carrying out load to thin plate duplicate
It tests, measures the stress of in-service thin plate under conditions of not destroying in-service thin plate using Lamb wave.
In order to make those skilled in the art more fully understand technical solution of the present invention, below in conjunction with attached drawing and specifically
Embodiment, explanation is described in detail to sheet stress measurement method and sheet stress measuring system of the invention.
The present invention provides a kind of sheet stress measurement method, and this method is led to mainly for the relatively small metalwork of thickness
Thickness is less than 6mm in normal situation, it is not limited to sheet metal；Sheet stress measurement method of the invention includes following step
It is rapid:
S1, the thin plate duplicate for obtaining in-service thin plate, thin plate duplicate and in-service thin plate shape having the same and material；
In-service thin plate is the component for needing to be measured stress, is located in the workpiece being currently being used, and is existed by the simulation of thin plate duplicate
Thin plate is used as a servant, both thin plate duplicate and in-service thin plate have similar mechanical property.
S2, loading experiment is made to thin plate duplicate, according to Lamb wave SiZero group velocity resonant frequency of mode and application stress
Relationship obtains Lamb wave SiZero group velocity of duplicate mode-stress parameters；Loading experiment needs to apply stress to thin plate duplicate,
When in thin plate there are when stress, will affect spread speed of the ultrasonic wave in thin plate, i.e., generation acoustoelastic effect；Thin plate is in difference
Stress condition under, there is different vibration to show identical Lamb wave；Correspondingly, under identical stress condition, apply
Different Lamb wave acquisition signals can be obtained in the excitation of different frequency.
Lamb wave SiZero group velocity resonant frequency of mode is in SiMode occur 1 group velocity point corresponding to frequency, i=1,2,
3 ... wait integers, pass through S1、S2、S3... distinguish different mode；Group velocity, which refers to, has certain characteristic on the envelope of one section of wave
Point spread speed, zero group velocity is the state that Lamb wave group velocity is zero.
Loading experiment is carried out to thin plate duplicate, thin plate, by Lamb wave, passes through load under conditions of different stress
Experiment can obtain Lamb wave S corresponding to the thin plate duplicate under different stress conditionsiIt zero group velocity resonant frequency of mode and applies
Add the relationship of stress.
After the relevant parameter for obtaining thin plate duplicate, step S3 is carried out, motivate blue nurse to a certain detection zone of in-service thin plate
Wave, and the receiving point near excitation point obtains Lamb wave and acquires signal；In-service thin plate keeps original state in this step, motivates blue nurse
Wave and the process for receiving Lamb wave carry out on the surface of in-service thin plate.
It obtains after Lamb wave acquires signal and carries out step S4, Lamb wave acquisition signal is handled, obtain Lamb wave mould
The in-service resonant frequency S of zero group velocity of stateif, according to the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate in-service thin plate detection zone
Mean stress suffered by domain.
The in-service resonant frequency S of zero group velocity of Lamb wave modeifIndicate that in-service template under its stress condition, is swashed by Lamb wave
Resonant frequency when encouraging.Using the above-mentioned loading experiment relevant parameter to thin plate duplicate and the resonant frequency of in-service thin plate,
This method can correspond to the mean stress for calculating detection zone under conditions of not destroying in-service thin plate using acoustoelastic effect.
On the basis of above scheme, the invention also includes following steps:
S5, mean stress is computed repeatedly to the different detection zones of in-service thin plate, describes the Stress Field Distribution of in-service thin plate
Figure；Step S5 is equivalent to the process of repeatedly step S4, the resonant frequency of in-service thin plate in different detection zones is obtained, by each
The resonant frequency of a detection zone draws Stress Field Distribution figure.Detection zone be Lamb wave excitation point with Lamb wave receiving point it
Between interval region.
Preferably, the present invention provides the specific embodiment that a kind of pair of thin plate duplicate carries out step S2 operation, such as Fig. 1 institute
Show, is the flow chart of sheet stress measurement method of the present invention, loading experiment step S2, is made to thin plate duplicate, obtain Lamb wave
SiZero group velocity of duplicate mode-stress parameters, specifically includes the following steps:
S21, Lamb wave signal is motivated to thin plate duplicate in excitation point, the receiving point in excitation twice of wave-length coverage of point
Acquire Lamb wave time-domain signal；The case where time-domain signal changes over time for wave.
S22, Hanning window function is added to Lamb wave time-domain signal, and carries out Fast Fourier Transform, obtain Lamb wave frequency
Domain signal waveforms；Lamb wave S is extracted from Lamb wave frequency-region signal waveform diagramiZero group velocity of mode thin plate in no applied stress
The corresponding Lamb wave S of duplicateiZero group velocity resonant frequency of mode；When carrying out the step, thin plate duplicate not by external force,
Inside is not because of the stress of external force generation.
S23, apply simple stress of different sizes several times to thin plate duplicate, simple stress is in elastic stress range
It is interior；After simple stress reaches stable state, Lamb wave S under each simple stress is obtainediZero group velocity resonant frequency of mode；Simple stress is
For the active force applied along straight line direction, when carrying out the step, simple stress is applied to thin plate duplicate several times, every time
When applying the simple stress of particular size, is kept for a period of time, after simple stress reaches stable state, repeat the above steps S22's
Process obtains Lamb wave S under each different size of simple stressiZero group velocity resonant frequency of mode.
S24, with Lamb wave SiZero group velocity resonant frequency of mode is abscissa, and simple stress is ordinate, establishes Descartes
Coordinate system；By simple stress and corresponding Lamb wave SiThe corresponding coordinate points of zero group velocity resonant frequency of mode substitute into coordinate system,
And linear fit is carried out to coordinate points, obtained straight slope K is Lamb wave SiZero group velocity of duplicate mode-stress parameters, directly
The intersection point of line and axis of abscissas is constant C.
Under identical stress condition, apply the excitation of different frequency, different Lamb wave acquisition signals can be obtained；And it is every
The corresponding resonant frequency of one simple stress namely zero group velocity point, amplitude reach maximum.As shown in Fig. 2, being frequency and amplitude
Between frequency-domain waveform figure, abscissa is frequency, and ordinate is amplitude；Solid line A indicates Lamb wave S in figureiMode is unstressed
Frequency-domain waveform figure in sheet metal plate；Dotted line B indicates Lamb wave SiMode is in by 200MPa simple stress sheet metal
Frequency-domain waveform figure；Dotted line C indicates Lamb wave SiMode is by the frequency-domain waveform figure in 400MPa simple stress sheet metal.In figure
Less than the corresponding frequency of wave crest, that is, Lamb wave S within the scope of cutoff frequencyiZero group velocity resonant frequency of mode.As we can see from the figure
With the increase for applying pulling force to sheet metal, Lamb wave Si1 group velocity point of mode is being moved to the left, and 1 group velocity point is corresponding total
Vibration frequency is also reducing.
Preferably, when making loading experiment to thin plate duplicate in the present invention, excitation point and the line of receiving point are answered with single shaft
The direction of power is parallel.
Further, the present invention provides the specific embodiment of step S4 a kind of herein, step S4, acquires and believes to Lamb wave
It number is handled, according to Lamb wave SiZero group velocity resonant frequency of mode calculates mean stress suffered by in-service thin plate detection zone,
It specifically includes with step:
S41, Hanning window function is added to Lamb wave acquisition signal, and carries out Fast Fourier Transform, obtain Lamb wave Si
Lamb wave mode zero group velocity in-service resonant frequency S of zero group velocity of mode in in-service thin plate detection zoneif.This step and step
Process conducted in S22 is similar, SifFor Lamb wave SiResonance frequency of zero group velocity of mode in in-service sheet metal detection zone
Rate.
S42, according to straight slope K, constant C, the in-service resonant frequency S of zero group velocity of Lamb wave modeif, utilize following formula meter
Calculate the mean stress of in-service thin plate detection zone:
σ=KSif-C
Wherein, σ is mean stress.
Concrete analysis process is as follows:
When there are when stress, will affect spread speed of the ultrasound in sheet metal, that is, being sent out in detected sheet metal
Raw acoustoelastic effect.Simple stress in sheet metal and longitudinal wave velocity that stress direction propagation is parallel in sheet metal
Relation equation are as follows:
Wherein, E is the elasticity modulus of material, unit Pa；L is sonoelastic coefficient, and V is biography of the longitudinal wave in sample
Speed is broadcast, unit is m/s；V0For spread speed of the longitudinal wave in unstressed thin plate duplicate, unit is m/s.
In sheet metal, Lamb wave S1The resonant frequency position that 1 group velocity point of mode occurs and velocity of longitudinal wave size in material
Governing equation it is as follows:
Wherein, S1fFor Lamb wave S1Mode generates corresponding resonant frequency when 1 group velocity point, and unit is Hz；β be one with
The related coefficient of the Poisson's ratio of material；V indicates velocity of longitudinal wave in material, and unit is m/s；D indicates plate thickness, and unit is m.
Simultaneous (1), (2) are it can be concluded that Lamb wave S1Mode generates corresponding resonant frequency and sheet metal institute when zero group velocity
It is as follows by stress relation formula:
In order to express conveniently, enable
The theoretical formula for finally obtaining the sheet metal stress field based on zero group velocity mode of Lamb wave is as follows:
σ=KS1f-C
Therefore, when sheet metal is by stress, Lamb wave S1Mode is corresponding zero group in metal target thin plate
Fast resonant frequency can occur to change accordingly, and zero group velocity resonant frequency and stress suffered by sheet metal are in a linear relationship.
The present invention also provides a kind of sheet stress measuring systems, as shown in figure 3, for sheet stress measuring system of the present invention
Structural schematic diagram；Including function generator 1, ultrasonic preamplifier 2, P wave emission probe 3, angle modifying wedges 4, indulge
The structures such as wave receiving transducer 5, ultrasonic post amplifier 6, oscillograph 7, processing module 8, stretching-machine 9；Function generator 1 is for sending out
Pulse electrical signal is penetrated, the pulse electrical signal that function generator 1 emits is broadcast to longitudinal wave after the processing of ultrasonic preamplifier 2
Transmitting probe 3, P wave emission probe 3 emits longitudinal wave to thin plate at an angle by angle modifying wedges 4, same in progress
When a experiment, the angle of angle modifying wedges 4 is kept fixed constant.
Longitudinal wave receiving transducer 5 receives the Lamb wave of thin plate, is sent to oscillograph 7 after the processing of ultrasonic post amplifier 6
It has been shown that, and by 8 calculation processing of processing module；Processing module 8 can be according to Lamb wave SiZero group velocity resonant frequency of mode and application
The relationship of stress obtains Lamb wave SiZero group velocity of duplicate mode-stress parameters；And Lamb wave acquisition signal is handled,
Obtain the in-service resonant frequency S of zero group velocity of Lamb wave modeif, according to the in-service resonant frequency S of zero group velocity of Lamb wave modeifIt calculates
Use as a servant mean stress suffered by thin plate detection zone；Mean stress is computed repeatedly to the different detection zones of in-service thin plate, is depicted in
Use as a servant the Stress Field Distribution figure of thin plate.It is complete by processing module 8 that analytical procedure is calculated involved in above-mentioned sheet stress measurement method
At.
It further include the stretching-machine 9 for applying simple stress to thin plate duplicate, it is as shown in the figure to indicate that two left and right sides are applied
Add lateral pulling force.
Specifically, P wave emission pops one's head in the distance between 3 and longitudinal wave receiving transducer 5 less than or equal to twice of wave in the present invention
It is long.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, this hair
It is bright to be not intended to be limited to the embodiments shown herein, and be to fit to and the principles and novel features disclosed herein phase
Consistent widest scope.
Claims (7)
1. a kind of sheet stress measurement method characterized by comprising
S1, the thin plate duplicate for obtaining in-service thin plate, the thin plate duplicate and in-service thin plate shape having the same and
Material；
S2, loading experiment is made to the thin plate duplicate, according to Lamb wave SiZero group velocity resonant frequency of mode and the pass for applying stress
System obtains Lamb wave SiZero group velocity of duplicate mode-stress parameters；
S3, signal is acquired to a certain area excitation Lamb wave of in-service thin plate, and motivating the receiving point near point to obtain Lamb wave；
S4, Lamb wave acquisition signal is handled, obtains the in-service resonant frequency S of zero group velocity of Lamb wave modeif, according to institute
State the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate mean stress suffered by in-service thin plate detection zone.
2. sheet stress measurement method according to claim 1, which is characterized in that further include:
S5, mean stress is computed repeatedly to the different detection zones of in-service thin plate, describes the Stress Field Distribution figure of in-service thin plate.
3. sheet stress measurement method according to claim 2, which is characterized in that step S2, to the thin plate duplicate
Make loading experiment, obtains Lamb wave SiZero group velocity of duplicate mode-stress parameters, comprising:
S21, Lamb wave signal is motivated to the thin plate duplicate in excitation point, the receiving point in excitation twice of wave-length coverage of point
Acquire Lamb wave time-domain signal；
S22, Hanning window function is added to the Lamb wave time-domain signal, and carries out Fast Fourier Transform, obtain Lamb wave frequency
Domain signal waveforms；Lamb wave S is extracted from the Lamb wave frequency-region signal waveform diagramiZero group velocity of mode is in no applied stress
The corresponding Lamb wave S of the thin plate duplicateiZero group velocity resonant frequency of mode；
S23, simple stress of different sizes is applied several times to the thin plate duplicate, the simple stress is in elastic stress model
In enclosing；After the simple stress reaches stable state, Lamb wave S under each simple stress is obtainediZero group velocity resonant frequency of mode；
S24, with Lamb wave SiZero group velocity resonant frequency of mode is abscissa, and simple stress is ordinate, establishes cartesian coordinate
System；By the simple stress and corresponding Lamb wave SiThe corresponding coordinate points of zero group velocity resonant frequency of mode substitute into coordinate system,
And linear fit is carried out to coordinate points, obtained straight slope K is the Lamb wave SiZero group velocity of duplicate mode-stress ginseng
The intersection point of number, straight line and axis of abscissas is constant C.
4. sheet stress measurement method according to claim 3, which is characterized in that it is real to make load to the thin plate duplicate
When testing, excitation point is parallel with the direction of the simple stress with the line of receiving point.
5. sheet stress measurement method according to claim 4, which is characterized in that step S4, acquired to the Lamb wave
Signal is handled, according to Lamb wave SiZero group velocity resonant frequency of mode calculates averagely answers suffered by in-service thin plate detection zone
Power, comprising:
S41, Hanning window function is added to Lamb wave acquisition signal, and carries out Fast Fourier Transform, obtain Lamb wave SiMould
Lamb wave mode zero group velocity in-service resonant frequency S of zero group velocity of state in in-service thin plate detection zoneif；
S42, according to the straight slope K, the constant C, the in-service resonant frequency S of zero group velocity of Lamb wave modeif, utilize with
Lower formula calculates the mean stress of in-service thin plate detection zone:
σ=KSif-C
Wherein, σ is mean stress.
6. a kind of sheet stress measuring system, which is characterized in that including the function generator (1) for emitting pulse electrical signal,
The pulse electrical signal of function generator (1) transmitting is broadcast to P wave emission after ultrasonic preamplifier (2) is handled and visits
Head (3), the P wave emission probe (3) emit longitudinal wave to thin plate at an angle by angle modifying wedges (4)；
Longitudinal wave receiving transducer (5) receives the Lamb wave of thin plate, is sent to oscillograph after ultrasonic post amplifier (6) processing
(7) it shows, and by processing module (8) calculation processing；
The processing module (8) can be according to Lamb wave SiZero group velocity resonant frequency of mode and the relationship for applying stress obtain blue nurse
Wave SiZero group velocity of duplicate mode-stress parameters；And Lamb wave acquisition signal is handled, obtain Lamb wave mode zero
The in-service resonant frequency S of group velocityif, according to the in-service resonant frequency S of zero group velocity of Lamb wave modeifCalculate in-service thin plate detection zone
Mean stress suffered by domain；Mean stress is computed repeatedly to the different detection zones of in-service thin plate, describes the stress of in-service thin plate
Field pattern；
It further include the stretching-machine (9) for applying simple stress to thin plate duplicate.
7. sheet stress measuring system according to claim 6, which is characterized in that the P wave emission probe (3) and institute
The distance between longitudinal wave receiving transducer (5) is stated less than or equal to twice of wavelength.
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| CN112326786A (en) * | 2020-10-16 | 2021-02-05 | 河北工业大学 | Metal plate stress detection method based on electromagnetic ultrasonic Lamb wave S1 modal group velocity |
| CN114878047A (en) * | 2022-04-29 | 2022-08-09 | 北京工业大学 | Water immersion type lamb wave collinear mixing detection system and method for residual stress detection in metal plate |
| CN114923442A (en) * | 2022-05-18 | 2022-08-19 | 南京理工大学 | Method and device for measuring thickness of each layer of double-layer thin plate based on ultrasonic Lamb wave zero group velocity resonance |
| CN115255509A (en) * | 2022-09-29 | 2022-11-01 | 中铝材料应用研究院有限公司 | Sheet cutting device for representing residual stress inside sheet |
| CN118730006A (en) * | 2024-09-04 | 2024-10-01 | 广东工业大学 | Method, device and system for measuring corrosion thickness of pipeline |
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